View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 22224U 92076F 24358.14632278 .00000176 00000-0 20044-3 0 9998
2 22224 70.9912 250.6260 0193538 32.8430 328.4525 13.74837451610124
| Epoch (UTC): | 23 December 2024 03:30:42 |
| Eccentricity: | 0.0193538 |
| inclination: | 70.9912° |
| perigee height: | 840 km |
| apogee height: | 1125 km |
| right ascension of ascending node: | 250.6260° |
| argument of perigee: | 32.8430° |
| revolutions per day: | 13.74837451 |
| mean anomaly at epoch: | 328.4525° |
| orbit number at epoch: | 61012 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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